AU4787200A - Translation and locking mechanism in missile - Google Patents

Translation and locking mechanism in missile

Info

Publication number
AU4787200A
AU4787200A AU47872/00A AU4787200A AU4787200A AU 4787200 A AU4787200 A AU 4787200A AU 47872/00 A AU47872/00 A AU 47872/00A AU 4787200 A AU4787200 A AU 4787200A AU 4787200 A AU4787200 A AU 4787200A
Authority
AU
Australia
Prior art keywords
rocket motor
missile
translation
locking mechanism
projectile
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU47872/00A
Inventor
Hans B. Biserod
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nammo Raufoss AS
Original Assignee
Nammo Raufoss AS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from NO19992739A external-priority patent/NO310379B1/en
Application filed by Nammo Raufoss AS filed Critical Nammo Raufoss AS
Publication of AU4787200A publication Critical patent/AU4787200A/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B15/00—Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/19—Pyrotechnical actuators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B15/00—Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
    • F15B15/20—Other details, e.g. assembly with regulating devices
    • F15B15/22—Other details, e.g. assembly with regulating devices for accelerating or decelerating the stroke
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/06—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with hard or heavy core; Kinetic energy penetrators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Analytical Chemistry (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

A translation and locking mechanism for a projectile that is lying in a standby position within a rocket motor in a missile, wherein the projectile is translated with respect to the rocket motor by means of a pyrotechnic charge before the rocket motor is ignited. The rear end of the projectile includes at least one radially spring biased lock and the front part of the rocket motor includes an internal circumferential groove that the at least one lock snaps into when the at least one lock is translated to the groove.
AU47872/00A 1999-06-04 2000-06-02 Translation and locking mechanism in missile Abandoned AU4787200A (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
NO19992739A NO310379B1 (en) 1999-06-04 1999-06-04 Deceleration and locking device for use between a projectile and a pilot fin in a missile
NO19992739 1999-06-04
NO19995141 1999-10-21
NO995141A NO308716B1 (en) 1999-06-04 1999-10-21 Missile forwarding and locking mechanism
PCT/NO2000/000190 WO2000075600A1 (en) 1999-06-04 2000-06-02 Translation and locking mechanism in missile

Publications (1)

Publication Number Publication Date
AU4787200A true AU4787200A (en) 2000-12-28

Family

ID=26648976

Family Applications (1)

Application Number Title Priority Date Filing Date
AU47872/00A Abandoned AU4787200A (en) 1999-06-04 2000-06-02 Translation and locking mechanism in missile

Country Status (9)

Country Link
US (1) US6640720B1 (en)
EP (1) EP1185836B1 (en)
AT (1) ATE315773T1 (en)
AU (1) AU4787200A (en)
DE (1) DE60025483T2 (en)
ES (1) ES2256007T3 (en)
IL (1) IL146921A0 (en)
NO (1) NO308716B1 (en)
WO (1) WO2000075600A1 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE518657C2 (en) * 2000-07-03 2002-11-05 Bofors Defence Ab Fine stabilized steerable projectile
US7262394B2 (en) * 2004-03-05 2007-08-28 The Boeing Company Mortar shell ring tail and associated method
US20070234925A1 (en) * 2004-09-07 2007-10-11 Dunn Robert H Sabot allowing .17-caliber projectile use in a .22-caliber weapon
EP2002198B1 (en) * 2006-03-30 2013-04-24 Raytheon Company Methods and apparatus for integrated locked thruster mechanism
US7700902B2 (en) * 2007-10-18 2010-04-20 Hr Textron, Inc. Locking assembly for rotary shafts
US8735789B1 (en) * 2010-09-20 2014-05-27 The United States Of America As Represented By The Secretary Of The Army Extendable stabilizer for projectile
RU2528473C2 (en) * 2012-11-29 2014-09-20 Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Assy for separation of aircraft compartments
RU2649433C1 (en) * 2017-02-20 2018-04-03 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Compartments separation node of the aircraft
RU2700643C1 (en) * 2018-08-31 2019-09-18 Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" Pyrofixator for docking and detachment of compartments of aircraft
US11624597B1 (en) 2021-03-25 2023-04-11 The United States Of America As Represented By The Secretary Of The Army Hybrid annular-cantilevered snap-fit joint
US11650034B1 (en) * 2021-03-25 2023-05-16 The United States Of America As Represented By The Secretary Of The Army Internal captive collar joint for projectile
CN114132532B (en) * 2022-01-12 2023-09-29 北京中科宇航技术有限公司 Landing leg mechanism for recovering rocket

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3256818A (en) * 1955-11-26 1966-06-21 Berghaus Bernhard Method of reducing barrel wear
US2936710A (en) * 1956-01-03 1960-05-17 Curtiss Wright Corp High mach deceleration device
US2935946A (en) * 1957-07-19 1960-05-10 Elia A Gallo Telescoping ram jet construction
US3086467A (en) * 1959-05-15 1963-04-23 John J Gallagher Gas operated extendible probe for ballistic model
US3071404A (en) * 1960-12-08 1963-01-01 Austin G Van Hove Explosively releasable fastener
US3160098A (en) * 1962-11-05 1964-12-08 William A Schulze Missile separation system
US3705550A (en) * 1970-11-02 1972-12-12 Us Army Solid rocket thrust termination device
FR2146552A5 (en) * 1971-07-19 1973-03-02 France Etat
US3754507A (en) * 1972-05-30 1973-08-28 Us Navy Penetrator projectile
IL65929A0 (en) * 1982-06-01 1984-04-30 Israel State Sub-caliber projectile
DE3327945A1 (en) * 1983-08-03 1985-02-21 Rheinmetall GmbH, 4000 Düsseldorf BULLET WITH A PAYLOAD PART AND A DRIVE PART
US4573412A (en) * 1984-04-27 1986-03-04 The United States Of America As Represented By The Secretary Of The Army Plug nozzle kinetic energy penetrator rocket
US4628821A (en) * 1985-07-05 1986-12-16 The United States Of America As Represented By The Secretary Of The Army Acceleration actuated kinetic energy penetrator retainer
US4964339A (en) 1987-12-23 1990-10-23 General Dynamics Corp., Pomona Division Multiple stage rocket propelled missile system
DE69129815T2 (en) 1990-01-16 1998-12-03 Tda Armements Sas Penetrator ammunition for targets with high mechanical resistance
US5892217A (en) * 1997-07-22 1999-04-06 Pollin; Irvin Lock and slide mechanism for tube launched projectiles

Also Published As

Publication number Publication date
WO2000075600A1 (en) 2000-12-14
US6640720B1 (en) 2003-11-04
DE60025483D1 (en) 2006-04-06
ATE315773T1 (en) 2006-02-15
EP1185836B1 (en) 2006-01-11
EP1185836A1 (en) 2002-03-13
ES2256007T3 (en) 2006-07-16
NO995141A (en) 2000-10-16
NO308716B1 (en) 2000-10-16
NO995141D0 (en) 1999-10-21
DE60025483T2 (en) 2006-09-14
IL146921A0 (en) 2002-08-14

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase